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<article article-type="research-article" dtd-version="1.0" specific-use="sps-1.6" xml:lang="en" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink">
	<front>
		<journal-meta>
			<journal-id journal-id-type="publisher-id">dyna</journal-id>
			<journal-title-group>
				<journal-title>DYNA</journal-title>
				<abbrev-journal-title abbrev-type="publisher">Dyna rev.fac.nac.minas</abbrev-journal-title>
			</journal-title-group>
			<issn pub-type="ppub">0012-7353</issn>
			<publisher>
				<publisher-name>Universidad Nacional de Colombia</publisher-name>
			</publisher>
		</journal-meta>
		<article-meta>
			<article-id pub-id-type="doi">10.15446/dyna.v85n205.62108</article-id>
			<article-categories>
				<subj-group subj-group-type="heading">
					<subject>Artículos</subject>
				</subj-group>
			</article-categories>
			<title-group>
				<article-title>Elastic behavior of stiffened curved plates subjected to transverse loading</article-title>
				<trans-title-group xml:lang="es">
					<trans-title>Comportamiento elástico de placas curvas rigidizadas sometidas a cargas transversales</trans-title>
				</trans-title-group>
			</title-group>
			<contrib-group>
				<contrib contrib-type="author">
					<name>
						<surname>Noguera-Garban</surname>
						<given-names>Abel</given-names>
					</name>
					<xref ref-type="aff" rid="aff1"><sup>a</sup></xref>
				</contrib>
				<contrib contrib-type="author">
					<name>
						<surname>Graciano</surname>
						<given-names>Carlos</given-names>
					</name>
					<xref ref-type="aff" rid="aff2"><sup>b</sup></xref>
				</contrib>
				<contrib contrib-type="author">
					<name>
						<surname>Zapata-Medina</surname>
						<given-names>David G.</given-names>
					</name>
					<xref ref-type="aff" rid="aff2"><sup>b</sup></xref>
				</contrib>
			</contrib-group>
			<aff id="aff1">
				<label>a</label>
				<institution content-type="original"> División de Ciencias Físicas y Matemáticas, Universidad Simón Bolívar, Venezuela. abel_noguera@yahoo.es</institution>
				<institution content-type="normalized">Universidad Simón Bolívar</institution>
				<institution content-type="orgdiv1">División de Ciencias Físicas y Matemáticas</institution>
				<institution content-type="orgname">Universidad Simón Bolívar</institution>
				<country country="VE">Venezuela</country>
				<email>abel_noguera@yahoo.es</email>
			</aff>
			<aff id="aff2">
				<label>b</label>
				<institution content-type="original"> Facultad de Minas, Universidad Nacional de Colombia, Medellín, Colombia. cagracianog@unal.edu.co, dgzapata@unal.edu.co</institution>
				<institution content-type="normalized">Universidad Nacional de Colombia</institution>
				<institution content-type="orgdiv1">Facultad de Minas</institution>
				<institution content-type="orgname">Universidad Nacional de Colombia</institution>
				<addr-line>
					<named-content content-type="city">Medellín</named-content>
				</addr-line>
				<country country="CO">Colombia</country>
				<email>cagracianog@unal.edu.co</email>
				<email>dgzapata@unal.edu.co</email>
			</aff>
			<pub-date pub-type="epub-ppub">
				<season>Apr-Jun</season>
				<year>2018</year>
			</pub-date>
			<volume>85</volume>
			<issue>205</issue>
			<fpage>83</fpage>
			<lpage>89</lpage>
			<history>
				<date date-type="received">
					<day>02</day>
					<month>02</month>
					<year>2017</year>
				</date>
				<date date-type="rev-recd">
					<day>01</day>
					<month>01</month>
					<year>2017</year>
				</date>
				<date date-type="accepted">
					<day>15</day>
					<month>02</month>
					<year>2018</year>
				</date>
			</history>
			<permissions>
				<license license-type="open-access" xlink:href="http://creativecommons.org/licenses/by-nc-nd/4.0/" xml:lang="en">
					<license-p>This is an open-access article distributed under the terms of the Creative Commons Attribution License</license-p>
				</license>
			</permissions>
			<abstract>
				<title>Abstract</title>
				<p>This paper presents a numerical study on the elastic behavior of stiffened curved plates subjected to transverse loading. The analyses are performed by means of linear static analysis using finite element modelling. Firstly, flat plates under transverse loading (uniform and non-uniform-trapezoidal) are modelled to validate the computational model against analytical solutions available in the literature. Secondly, the behavior of unstiffened curves plates under transverse loading is analyzed. Then, the influence of both, transversal and longitudinal stiffening in controlling the out-of-plane displacements and stresses distribution of the curve plates is demonstrated. Finally, a case-study concerning the response of a hydroelectric power plant intake gates subjected to a hydrostatic head is further investigated. The results show that the increase in gate stiffness is reflected in smaller deformations implying a better performance and system integrity.</p>
			</abstract>
			<trans-abstract xml:lang="es">
				<title>Resumen</title>
				<p>Este trabajo presenta un estudio numérico del comportamiento elástico de placas curvas rigidizadas sometidas a carga transversal. Los análisis se realizaron mediante análisis estático lineal utilizando modelación por elementos finitos. Inicialmente, placas planas bajo carga transversal (uniforme y no uniforme-trapezoidal) se modelan para validar el modelo computacional frente a soluciones analíticas disponibles en la literatura. En segundo lugar, se analiza el comportamiento de las placas curvas no rigidizadas bajo carga transversal. Luego, se demuestra la influencia de la rigidez longitudinal y transversal en el control de la distribución de desplazamientos y tensiones fuera de plano de las placas curvas. Finalmente, la respuesta de una compuerta radial de una planta hidroeléctrica sometida a una cabeza hidrostática es investigada. Los resultados muestran que el aumento en la rigidez a la puerta se refleja en las deformaciones más pequeñas lo que implica un mejor rendimiento y la integridad del sistema.</p>
			</trans-abstract>
			<kwd-group xml:lang="en">
				<title>Keywords:</title>
				<kwd>curved plates</kwd>
				<kwd>stiffeners</kwd>
				<kwd>finite elements</kwd>
				<kwd>intake gates</kwd>
				<kwd>hydrostatic head</kwd>
				<kwd>deformations</kwd>
			</kwd-group>
			<kwd-group xml:lang="es">
				<title>Palabras clave:</title>
				<kwd>placas curvas</kwd>
				<kwd>rigidizadores</kwd>
				<kwd>elementos finitos</kwd>
				<kwd>compuertas</kwd>
				<kwd>carga hidrostática</kwd>
				<kwd>deformaciones</kwd>
			</kwd-group>
			<counts>
				<fig-count count="17"/>
				<table-count count="4"/>
				<equation-count count="7"/>
				<ref-count count="20"/>
				<page-count count="7"/>
			</counts>
		</article-meta>
	</front>
	<body>
		<sec sec-type="intro">
			<title>1. Introduction</title>
			<p>Curved plate elements have traditionally been used in mechanical, aeronautical and marine/off-shore engineering. These structural elements are found in the fuselage of aircrafts, oil and gas storage structures, cooling towers and ship hulls. Their applications in civil engineering are relatively recent and mainly focus on the construction of steel bridges. Typical examples of curved panels in bridge engineering are orthotropic decks in box-girder bridges and webs of in-plane curved I-girders.</p>
			<p>Stiffened curved plates are also becoming more and more popular as recent developments of the curving process allow for a faster and more economic manufacturing. Nevertheless, their design is complex and difficult due to the lack of standard building code specifications [<xref ref-type="bibr" rid="B1">1</xref>], few studies related to their stability are available in the literature [<xref ref-type="bibr" rid="B2">2</xref>-<xref ref-type="bibr" rid="B4">4</xref>]. Consequently, curved plate analysis and design rely significantly on expensive and time-consuming finite element modeling [<xref ref-type="bibr" rid="B2">2</xref>,<xref ref-type="bibr" rid="B3">3</xref>].</p>
			<p>Recently, the influence of longitudinal stiffening on both, critical and ultimate strength of plate girders has been investigated [<xref ref-type="bibr" rid="B5">5</xref>-<xref ref-type="bibr" rid="B7">7</xref>]. The primary function of the stiffeners is to control out-of-plane displacements of the thin-walled webs and increase bending resistance.</p>
			<p>This paper presents a numerical investigation on the elastic behavior of stiffened curved plates subjected to transversal loading. A parametric study is performed through finite element analysis to evaluate the beneficial effects of including longitudinal and transverse stiffeners on the performance of curved plates. Firstly, the numerical model is validated against theoretical formulae available in the literature. Then, a case study is further analyzed to evaluate the response of a hydroelectric power plant intake radial gate subjected to a hydrostatic head. At the end, the results show that stiffeners are a practical way to retrofit existing structural elements as they increase the system stiffness and reduce transversal deformations, which is directly reflected in an improvement of system reliability.</p>
		</sec>
		<sec>
			<title>2. Numerical modeling</title>
			<p>This section presents a numerical study conducted to investigate the influence of transversal and longitudinal stiffening on the out-of-plane displacements of stiffened curved plates subjected to transverse loading.</p>
			<p>Various computational models for plates under transversal loading are elaborated using the finite element software ANSYS [<xref ref-type="bibr" rid="B8">8</xref>]. A detailed description of the employed numerical models can be found in [<xref ref-type="bibr" rid="B9">9</xref>]. These models are validated using a procedure that considers the influence of the plate geometry (flat and curved), boundary and loading conditions and finally considering the presence of transverse and longitudinal stiffening. Thereafter, a more complex numerical model is elaborated to investigate the influence of the stiffening on the out-of-plane displacements and stress distribution of a curved plate.</p>
			<p>The material used in all analyses is an ASTM A516 Gr 70 steel, with Young’s modulus, E= 206 GPa; Poisson ratio, 𝜐= 0.3; density, 𝛾= 7.85×10<sup>-6</sup> kg/m<sup>3</sup>; yield strength, 𝑓 𝑦 = 260 MPa and ultimate strength 𝑓 𝑢 = 485 MPa.</p>
			<sec>
				<title>2.1. Flat plates under transverse loading</title>
				<p>As mentioned above, the first step into the validation procedure of the numerical methodology is to investigate the influence of boundary and loading conditions on the structural response of flat plates subjected to transverse loading. In this regard, <xref ref-type="table" rid="t1">Table 1</xref> shows a schematic view of boundary and loading conditions for the three numerical models developed for flat plates herein: Model N1 with the upper and lower ends free to move and the lateral ends simply supported, under uniform transverse loading (𝑝 = 0.001 MPa); Model N2 with the upper and lower ends free to move and the lateral ends simply supported, under non-uniform (trapezoidal) transverse loading (𝑝 = 0.01667 MPa); and Model N3 clamped at four ends, under uniform transverse loading (𝑝 = 0.001 MPa).</p>
				<p>
					<table-wrap id="t1">
						<label>Table 1</label>
						<caption>
							<title>Flat plate models.</title>
						</caption>
						<graphic xlink:href="0012-7353-dyna-85-205-00083-gt1.jpg"/>
						<table-wrap-foot>
							<fn id="TFN1">
								<p><bold>Source:</bold> The authors.</p>
							</fn>
						</table-wrap-foot>
					</table-wrap>
				</p>
				<p>
					<xref ref-type="table" rid="t1">Table 1</xref> also shows formulas for the calculation of maximum stresses 𝜎 𝑚𝑎𝑥 and displacements 𝛿 𝑚𝑎𝑥 [<xref ref-type="bibr" rid="B10">10</xref>]. Shell181 elements from the ANSYS element library [<xref ref-type="bibr" rid="B8">8</xref>] were used to model the plates. The dimensions of the plates were: width, 𝑏 1 = 10000 mm; height, 𝑎 1 = 10000 mm; and thickness, 𝑡 𝑝 = 20 mm (see <xref ref-type="fig" rid="f1">Fig. 1a</xref>). An additional parametric study was conducted regarding the panel aspect ratio, 𝛼= 𝑏 1 / 𝑎 1 = 1.5, 2 and 2.5, maintaining constant the height, 𝑎 1 = 10000 mm. <xref ref-type="fig" rid="f1">Fig. 1b</xref> shows a representative mesh of the flat plates, while <xref ref-type="fig" rid="f2">Figs. 2a</xref> and <xref ref-type="fig" rid="f2">2b</xref> show the out-of-plane displacements plots obtained numerically for Models N1 and N2, respectively.</p>
				<p>
					<fig id="f1">
						<label>Figure 1</label>
						<caption>
							<title>(a) Dimensions for Models N1, N2 and N3, and (b) Mesh for flat plates. </title>
						</caption>
						<graphic xlink:href="0012-7353-dyna-85-205-00083-gf1.jpg"/>
						<attrib><bold>Source:</bold> The authors.</attrib>
					</fig>
				</p>
				<p>
					<fig id="f2">
						<label>Figure 2</label>
						<caption>
							<title>Radial displacement with 𝑝 = 0.001 MPa and 𝛼=1: (a) Model N1 and (b) Model N2. </title>
						</caption>
						<graphic xlink:href="0012-7353-dyna-85-205-00083-gf2.jpg"/>
						<attrib><bold>Source:</bold> The authors.</attrib>
					</fig>
				</p>
				<p>
					<xref ref-type="fig" rid="f3">Fig. 3</xref> shows a comparison for maximum displacements and stresses, between computed values and those obtained analytically with the equations proposed by [<xref ref-type="bibr" rid="B10">10</xref>] and summarized in <xref ref-type="table" rid="t1">Table 1</xref>. A good agreement between numerical and analytical results is achieved with a maximum difference of approximately 10%. It is worth noticing that the available formulas were obtained for stresses and displacements in the elastic range. Even though, the stresses are slightly higher than the corresponding yield strength of the material ( 𝑓 𝑦 = 260 MPa). The figure shows that for Model N1 the maximum radial displacement increases with the panel aspect ratio, 𝛼. For Model N2, with the same boundary conditions as Model N1 but different load distribution, the maximum radial displacement reduces about 30% compared to Model N1. For Model N3, clamped in all ends and uniformly loaded, the maximum displacement is reduced around 50% with regards to Model N1. These results demonstrate the impact of boundary and loading conditions on both, maximum displacements and maximum stress when modeling flat plates subjected to transverse loading. The results also show that both, the maximum displacement and the maximum stress increases with the panel aspect ratio for the three Models (N1, N2 and N3).</p>
				<p>
					<fig id="f3">
						<label>Figure 3</label>
						<caption>
							<title>Maximum radial displacement at the center of the plate and maximum von Mises stress intensity for Models N1, N2 and N3.</title>
						</caption>
						<graphic xlink:href="0012-7353-dyna-85-205-00083-gf3.jpg"/>
						<attrib><bold>Source:</bold> The authors.</attrib>
					</fig>
				</p>
			</sec>
			<sec>
				<title>2.2. Curved plates under transverse loading</title>
				<p>Continuing the methodology applied for flat plates, this section aims at investigating the influence of boundary and loading conditions on the structural response of curved plates subjected to transverse loading. Four additional models were developed as shown in <xref ref-type="fig" rid="f4">Fig. 4</xref>, hence: Model N4 with the upper and lower ends free to move and the lateral ends simply supported, under uniform transverse loading (𝑝= 0.1 MPa); Model N5 with the upper and lower ends free to move and the lateral ends simply supported, under non-uniform (trapezoidal) transverse loading (𝑝 = 0.1 MPa); Model N6 clamped at four ends, under uniform transverse loading (𝑝= 0.1 MPa); and Model N7 clamped at four ends, under non-uniform (trapezoidal) transverse loading (𝑝 = 0.1 MPa).</p>
				<p>
					<fig id="f4">
						<label>Figure 4</label>
						<caption>
							<title>Curve plate models. </title>
						</caption>
						<graphic xlink:href="0012-7353-dyna-85-205-00083-gf4.jpg"/>
						<attrib><bold>Source:</bold> The authors.</attrib>
					</fig>
				</p>
				<p>
					<xref ref-type="fig" rid="f4">Fig. 4</xref> shows a schematic view of boundary and loading conditions of the four models. Shell 181 elements from the ANSYS element library [<xref ref-type="bibr" rid="B8">8</xref>] were also used to model the plates. The dimensions of the plates were: width, 𝑏 2 = 10000 mm; height, 𝑎 2 = 10000 mm; plate radius, 𝑟= 9500 mm; and thickness, 𝑡 𝑝 = 10 mm. The panel aspect ratio, 𝛼= 𝑏 2 / 𝑎 2 (see <xref ref-type="fig" rid="f5">Fig. 5a</xref>), was varied as 𝛼= 1, 1.5, 2 and 2.5 maintaining constant the height, 𝑎 2 = 10000 mm. <xref ref-type="fig" rid="f5">Fig. 5b</xref> shows a representative mesh of the modeled curved plates.</p>
				<p>
					<fig id="f5">
						<label>Figure 5</label>
						<caption>
							<title>(a) Dimensions for Models N4, N5, N6 and N7; and (b) Meshing for the curved plates. </title>
						</caption>
						<graphic xlink:href="0012-7353-dyna-85-205-00083-gf5.jpg"/>
						<attrib><bold>Source:</bold> The authors.</attrib>
					</fig>
				</p>
				<p>Regarding the influence of the loading conditions, <xref ref-type="fig" rid="f6">Fig. 6</xref> shows a comparison between numerical results of the out-of-plane displacements for Models N4, N5, N6 and N7. In these cases, the radial displacement decreases when the panel aspect ratio increases, for both conditions, simply supported (<xref ref-type="fig" rid="f6">Fig. 6a</xref>) and fully clamped (<xref ref-type="fig" rid="f6">Fig. 6b</xref>). The reduction in the magnitude of the displacement between the former and the latter is close to 30%. When comparing the displacements for the two loading types with same boundary conditions the obtained difference is abou10%.</p>
				<p>
					<fig id="f6">
						<label>Figure 6</label>
						<caption>
							<title>Maximum radial displacement, 𝛿 𝑚𝑎𝑥 , with 𝑝 = 0.1 MPa. (a) Models N4 and N5 (b) Models N6 and N7. </title>
						</caption>
						<graphic xlink:href="0012-7353-dyna-85-205-00083-gf6.jpg"/>
						<attrib><bold>Source:</bold> The authors.</attrib>
					</fig>
				</p>
			</sec>
			<sec>
				<title>2.3. Stiffened curved plates under transverse loading</title>
				<p>In this section, a third parametric study is conducted to investigate the influence of transversal and longitudinal stiffening on the maximum out-of-plane displacement of curved plates. At this stage, it is important to quote that simply supported and trapezoidal loadings are the corresponding boundary and loading conditions for curved plates. Hence, the current analysis is performed taking into account these conditions. Hot-rolled profiles are currently used in the steel industry to stiffen plated structures.</p>
				<p>The geometry parameters of four (4) IPN steel profiles, namely IPN100, IPN180, IPN240 and IPN300 used in this study, are listed in <xref ref-type="table" rid="t2">Table 2</xref>. <xref ref-type="fig" rid="f7">Fig. 7</xref> shows the corresponding numerical models for different number of transversal stiffeners and <xref ref-type="fig" rid="f8">Fig. 8</xref> presents the results for the maximum radial displacements in the plane of symmetry of the curved plate considering the different profiles. As expected, the stiffener with the largest second moment of area (IPN300) gives the largest reduction in out-of-plane displacements of the curved plate.</p>
				<p>
					<table-wrap id="t2">
						<label>Table 2</label>
						<caption>
							<title>Geometry of the IPN steel profiles.</title>
						</caption>
						<graphic xlink:href="0012-7353-dyna-85-205-00083-gt2.jpg"/>
						<table-wrap-foot>
							<fn id="TFN2">
								<p><bold>Source:</bold> The authors.</p>
							</fn>
						</table-wrap-foot>
					</table-wrap>
				</p>
				<p>
					<fig id="f7">
						<label>Figure 7</label>
						<caption>
							<title>Models considering transversal stiffening (n = 2, 4, 6 and 8 stiffeners). </title>
						</caption>
						<graphic xlink:href="0012-7353-dyna-85-205-00083-gf7.png"/>
						<attrib><bold>Source:</bold> The authors.</attrib>
					</fig>
				</p>
				<p>
					<fig id="f8">
						<label>Figure 8</label>
						<caption>
							<title>Maximum radial displacement 𝛿 𝑚𝑎𝑥 in the plane of symmetry of the curved plate (n = 2, 4, 6 y 8 transversal stiffeners). </title>
						</caption>
						<graphic xlink:href="0012-7353-dyna-85-205-00083-gf8.jpg"/>
						<attrib><bold>Source:</bold> The authors.</attrib>
					</fig>
				</p>
				<p>To complete the study regarding the effect of stiffening on the deflection of curved plates, it is necessary to investigate the combined case with transversal and longitudinal stiffening.</p>
				<p>In this analysis, only one stiffener IPN100 was considered in the study. The number of the stiffeners in both directions was varied in both, the transverse direction (n= 3, 4, 6 and 8) and longitudinal direction (m= 4, 6 and 8). <xref ref-type="fig" rid="f9">Fig. 9</xref> shows a model with seven stiffeners, four in the longitudinal and three in the transversal direction. Boundary and loading conditions are the same as in the previous case.</p>
				<p>
					<fig id="f9">
						<label>Figure 9</label>
						<caption>
							<title>Model considering combined stiffening (longitudinal m = 4 and transversal n = 3). </title>
						</caption>
						<graphic xlink:href="0012-7353-dyna-85-205-00083-gf9.png"/>
						<attrib><bold>Source:</bold> The authors.</attrib>
					</fig>
				</p>
				<p>
					<xref ref-type="fig" rid="f10">Fig. 10</xref> shows the results for the maximum radial displacement achieved with the stiffener’s combinations investigated. It is observed that the radial displacements are reduced significantly for 8 longitudinal stiffeners. A reduction of 20% in the radial displacement is observed in <xref ref-type="fig" rid="f10">Fig. 10</xref>, when compared to the corresponding displacements for only transversal stiffeners. Obviously, a larger displacement reduction may be achieved by using larger stiffeners.</p>
				<p>
					<fig id="f10">
						<label>Figure 10</label>
						<caption>
							<title>Maximum radial displacement for the combined stiffening model. </title>
						</caption>
						<graphic xlink:href="0012-7353-dyna-85-205-00083-gf10.jpg"/>
						<attrib><bold>Source:</bold> The authors.</attrib>
					</fig>
				</p>
			</sec>
		</sec>
		<sec>
			<title>3. Applications</title>
			<p>Intake gates are among the main elements regarding dam safety in a hydroelectric power plant as they control water levels in the reservoir. When the water level rises, the pressure on the gates increases and excessive deformations can take place compromising the safety of the reservoir [<xref ref-type="bibr" rid="B11">11</xref>-<xref ref-type="bibr" rid="B13">13</xref>]. In many cases, intake gate systems have surpassed the service life for which they were designed for the original operating conditions, such as hydrostatic load, opening and closing frequency, among others, have been significantly modified to meet new energy generation requirements. All this is reflected on structural changes of intake gates and their possible failure, which can yield the electric plant unserviceable and in some cases the collapse of the reservoir. That is precisely why intake gate systems require rehabilitation works to improve their operation and adapt to current operating requirements.</p>
			<p>In this section, the performance of the intake radial gates of the Antonio José de Sucre - Macagua I Hydroelectric Power Plant [<xref ref-type="bibr" rid="B14">14</xref>] is investigated. For this particular case, the intake radial gates were originally designed to withstand a hydrostatic head at an elevation of 48.0 m.s.n.m. In recent years, the water level of the reservoir was raised to 54.5 m.s.n.m. to accommodate for the increase in energy demand [<xref ref-type="bibr" rid="B15">15</xref>]. This increase in the level of the reservoir resulted in large gate deformations causing excessive water loss.</p>
			<p>
				<xref ref-type="fig" rid="f11">Fig. 11</xref> shows a picture of the radial gate of the Antonio José de Sucre - Macagua I Hydroelectric Power Plant and its main structural components. <xref ref-type="table" rid="t3">Table 3</xref> lists the geometry and dimensions of the radial gate. Due to symmetry in load and boundary conditions only one-half of the gate is modeled as shown in <xref ref-type="fig" rid="f12">Fig. 12</xref>. The longitudinal and vertical stiffeners were modeled using BEAM44 elements from the ANSYS element library [<xref ref-type="bibr" rid="B8">8</xref>]. Accordingly, the plate in the gate was modeled using SHELL 181 elements, the remaining parts were modeled with SOLID 187 elements. Also included in the figure are the boundary conditions used in the numerical model for the radial gate. In the middle, a symmetry line was established, the other ends of the gate were simply supported. In the horizontal beam, clamped conditions were used to consider the support provided by three stiff arms that maintain the gate in place.</p>
			<p>
				<fig id="f11">
					<label>Figure 11</label>
					<caption>
						<title>Radial gate of the Antonio José de Sucre - Macagua I Hydroelectric Power Plant. </title>
					</caption>
					<graphic xlink:href="0012-7353-dyna-85-205-00083-gf11.png"/>
					<attrib><bold>Source:</bold> [<xref ref-type="bibr" rid="B9">9</xref>].</attrib>
				</fig>
			</p>
			<p>
				<table-wrap id="t3">
					<label>Table 3</label>
					<caption>
						<title>Radial gate actual geometry and dimensions.</title>
					</caption>
					<graphic xlink:href="0012-7353-dyna-85-205-00083-gt3.jpg"/>
					<table-wrap-foot>
						<fn id="TFN3">
							<p><bold>Source:</bold> The authors.</p>
						</fn>
					</table-wrap-foot>
				</table-wrap>
			</p>
			<p>
				<fig id="f12">
					<label>Figure 12</label>
					<caption>
						<title>Model geometry and boundary conditions considering symmetry. </title>
					</caption>
					<graphic xlink:href="0012-7353-dyna-85-205-00083-gf12.jpg"/>
					<attrib><bold>Source:</bold> The authors.</attrib>
				</fig>
			</p>
			<p>After conducting a convergence analysis, a mesh with 142.593 elements was chosen. <xref ref-type="fig" rid="f13">Fig. 13</xref> shows the meshing used in the main supporting elements and the radial panel.</p>
			<p>
				<fig id="f13">
					<label>Figure 13</label>
					<caption>
						<title>Meshing used in the gate. </title>
					</caption>
					<graphic xlink:href="0012-7353-dyna-85-205-00083-gf13.png"/>
					<attrib><bold>Source:</bold> The authors.</attrib>
				</fig>
			</p>
			<p>In practice, radial gates sustain high transversal loadings due to the hydrostatic pressure gradient. Its determination is precisely the first step to adequately size a radial gate [<xref ref-type="bibr" rid="B16">16</xref>]. An upper bound for the hydrostatic pressure gradient acting on the gate can be defined using the maximum expected water level of the reservoir as shown in <xref ref-type="fig" rid="f14">Fig. 14</xref>.</p>
			<p>
				<fig id="f14">
					<label>Figure 14</label>
					<caption>
						<title>Hydrostatic pressure distribution assumed for the gate.</title>
					</caption>
					<graphic xlink:href="0012-7353-dyna-85-205-00083-gf14.jpg"/>
					<attrib><bold>Source:</bold> Adapted from [<xref ref-type="bibr" rid="B12">12</xref>].</attrib>
				</fig>
			</p>
			<p>The magnitude of the resultant hydrostatic load, 𝑊, can be found as:</p>
			<p>
				<disp-formula id="e1">
					<graphic xlink:href="0012-7353-dyna-85-205-00083-e1.png"/>
				</disp-formula>
			</p>
			<p>
				<disp-formula id="e2">
					<graphic xlink:href="0012-7353-dyna-85-205-00083-e2.png"/>
				</disp-formula>
			</p>
			<p>
				<disp-formula id="e3">
					<graphic xlink:href="0012-7353-dyna-85-205-00083-e3.jpg"/>
				</disp-formula>
			</p>
			<p>where 𝛼 𝑠 = 𝑠i𝑛 −1 ( 𝐷 𝑠 /𝑅), 𝛼 𝑖 = 𝑠𝑖𝑛 −1 ( 𝐷 𝑖 /𝑅), 𝐻 is the maximum expected water level of the reservoir, ℎ 1 is the depth to the radial gate, ℎ is the height of the gate, 𝐵 is the width of the gate, 𝑅 is the radius of the gate, 𝛾 𝑤 is the specific weight of water and 𝐷 𝑚 is depth to the point of curvature of the gate. The line of action of the resultant hydrostatic load on radial gates is assumed to pass through the point of curvature of the gate [<xref ref-type="bibr" rid="B16">16</xref>] at an orientation:</p>
			<p>
				<disp-formula id="e4">
					<graphic xlink:href="0012-7353-dyna-85-205-00083-e4.png"/>
				</disp-formula>
			</p>
			<p>Based on the above loading conditions, two design conditions arise: large displacements at the supported ends and high stress levels. As mentioned earlier, the situation may be solved by stiffening the gate by adding either transverse, longitudinal of both types of stiffeners.</p>
			<p>The maximum stress in a radial gate [<xref ref-type="bibr" rid="B17">17</xref>] can be estimated as:</p>
			<p>
				<disp-formula id="e5">
					<graphic xlink:href="0012-7353-dyna-85-205-00083-e5.png"/>
				</disp-formula>
			</p>
			<p>where 𝑘 is a dimensionless parameter that depends on the ratio 𝑏/𝑎 and on the boundary conditions ( 𝑘=25 [<xref ref-type="bibr" rid="B18">18</xref>]), 𝑝 is the hydrostatic pressure at the middle of the gate, 𝑡 is the plate thickness and 𝑎 and 𝑏 are the minimum and maximum spacing between stiffeners, respectively.</p>
			<p>The maximum deflection of the radial gate can be determined as:</p>
			<p>
				<disp-formula id="e6">
					<graphic xlink:href="0012-7353-dyna-85-205-00083-e6.jpg"/>
				</disp-formula>
			</p>
			<p>where 𝐸 is the Young’s modulus and 𝜉 is a dimensionless parameter that depends on the dimensions of the gate (see <xref ref-type="table" rid="t4">Table 4</xref>). For this specific case, 𝜉 was assumed equal to 0.0284.</p>
			<p>
				<table-wrap id="t4">
					<label>Table 4</label>
					<caption>
						<title>Dimensionless parameter ξ </title>
					</caption>
					<graphic xlink:href="0012-7353-dyna-85-205-00083-gt4.jpg"/>
					<table-wrap-foot>
						<fn id="TFN4">
							<p><bold>Source:</bold> Adapted from [<xref ref-type="bibr" rid="B19">19</xref>].</p>
						</fn>
					</table-wrap-foot>
				</table-wrap>
			</p>
			<p>
				<xref ref-type="disp-formula" rid="e5">Eqs. (5)</xref> and <xref ref-type="disp-formula" rid="e6">(6)</xref> provide the maximum values for stresses and displacements, respectively. After substituting the corresponding values into these formulas, a maximum stress of 𝜎 𝑚𝑎𝑥 =200 MPa and a maximum deflection 𝛿 𝑚𝑎𝑥 = 5.5 mm are obtained for the considered gate. It must be mentioned that these values represent operational conditions.</p>
			<p>
				<xref ref-type="fig" rid="f15">Fig. 15</xref> shows the displacement profile at the upper end of the gate. Note that a good agreement is obtained between the numerical results and the actual measurements [<xref ref-type="bibr" rid="B20">20</xref>]. From a practical point of view a maximum displacement of 22 mm means that the gate is leaking as such displacement goes beyond the allowable value of 5.5 mm.</p>
			<p>
				<fig id="f15">
					<label>Figure 15</label>
					<caption>
						<title>Displacement profile in the upper end of the gate.</title>
					</caption>
					<graphic xlink:href="0012-7353-dyna-85-205-00083-gf15.jpg"/>
					<attrib><bold>Source:</bold> The authors.</attrib>
				</fig>
			</p>
			<p>Taking into account that the maximum stress and the maximum displacement control the integrity of the gate and keeping in mind that the current design allows greater values for these parameters, it is necessary to solve this situation by adding stiffeners. Then, a parametric analysis using a simplified finite element model is conducted in order to reduce the maximum stress and the maximum displacement in the gate. In the simplified model, the arms are correspondingly substituted by a fixed boundary condition.</p>
			<p>In general, the flexural rigidity of the stiffener, 𝛾 𝑠 , is used to describe the capacity of a stiffener to resist buckling and control lateral deflection. Usually, this rigidity is expressed relative to the plate stiffness, 𝐷, as follows: </p>
			<p>
				<disp-formula id="e7">
					<graphic xlink:href="0012-7353-dyna-85-205-00083-e7.png"/>
				</disp-formula>
			</p>
			<p>where 𝐷=𝐸 𝑡 𝑤 3 /12 1− 𝜈 2 is the flexural rigidity of a unit width of the web plate. The flexural stiffness for the IPN profiles is also listed in <xref ref-type="table" rid="t2">Table 2</xref>.</p>
			<p>
				<xref ref-type="fig" rid="f16">Fig. 16</xref> shows the maximum displacements and stresses attained for the radial gate with stiffeners in both directions. These results are presented for the gate stiffened with IPN100 (<xref ref-type="fig" rid="f16">Figs. 16a</xref> and <xref ref-type="fig" rid="f16">16b</xref>) and IPN300 (<xref ref-type="fig" rid="f16">Figs. 16c</xref> and <xref ref-type="fig" rid="f16">16d</xref>). The distribution of the stiffeners was even in both directions. There is a reduction in the out-of-plane displacements of the gate after increasing the number of stiffeners, as well as after increasing the size of the stiffener. Similar results are observed for the maximum stresses. All the structural elements (plate and stiffeners) are subjected to bending, therefore an increase in the second moment of area of the stiffener leads to redistribution of the stresses in the gate, attaining a significant reduction.</p>
			<p>
				<fig id="f16">
					<label>Figure 16</label>
					<caption>
						<title>Maximum von Mises stress and maximum displacement at the supported ends from numerical simulations for profiles IPN 100 and 300.</title>
					</caption>
					<graphic xlink:href="0012-7353-dyna-85-205-00083-gf16.jpg"/>
					<attrib><bold>Source:</bold> The authors.</attrib>
				</fig>
			</p>
			<p>
				<xref ref-type="fig" rid="f17">Fig. 17</xref> shows the maximum displacements for the gate with 8 longitudinal and 8 transversal stiffeners. It is observed that an increasing flexural rigidity reduces the out-of-plate displacements. Comparing these results with the maximum allowable displacement found from <xref ref-type="disp-formula" rid="e6">Eq. (6)</xref> ( 𝛿 𝑚𝑎𝑥 = 5.5 mm) it is seen that the IPN300 stiffener is the only one capable of reducing the displacements below this limit.</p>
			<p>
				<fig id="f17">
					<label>Figure 17</label>
					<caption>
						<title>Maximum displacement in the gate with 8 longitudinal and 8 transverse stiffeners.</title>
					</caption>
					<graphic xlink:href="0012-7353-dyna-85-205-00083-gf17.png"/>
					<attrib><bold>Source:</bold> The authors.</attrib>
				</fig>
			</p>
		</sec>
		<sec sec-type="conclusions">
			<title>4. Summary and conclusions</title>
			<p>This paper has presented a numerical study on the elastic behavior of stiffened curved plates subjected to transverse loading; a parametric analysis to evaluate the beneficial effects of including longitudinal and transverse stiffeners; and the application of the proposed methodology to the specific case of radial intake gates in a hydroelectric power plant. The computational model was validated with analytical solutions available in the literature for flat and curved plates and by comparing it with a case history concerning the response of a hydroelectric power plant intake radial gate subjected to a hydrostatic head. It is shown that the static behavior of a curved plate subjected to hydrostatic head is a suitable way to size intake gates and define the maximum reservoir water level; and that stiffeners are a practical way to retrofit existing elements as they increase system stiffness and reduce transversal deformations, which are directly reflected in an improvement of system reliability and capacity to meet new power generation requirements.</p>
		</sec>
	</body>
	<back>
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		<fn-group>
			<fn fn-type="other" id="fn1">
				<label>How to cite:</label>
				<p> Noguera-Garban, A., Graciano, C. and Zapata-Medina, D.G., Elastic behavior of stiffened curved plates subjected to transverse loading. DYNA, 85(205), pp. 83-89, June, 2018.</p>
			</fn>
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	</back>
</article>